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A compression ignition engine uses two or more fuel charges having two or more reactivities to control the timing and duration of combustion. In a preferred implementation, a lower-reactivity fuel charge is injected or otherwise introduced into the combustion chamber, preferably sufficiently early t

A compression ignition engine uses two or more fuel charges having two or more reactivities to control the timing and duration of combustion. In a preferred implementation, a lower-reactivity fuel charge is injected or otherwise introduced into the combustion chamber, preferably sufficiently early that it becomes at least substantially homogeneously dispersed within the chamber before a subsequent injection is made. One or more subsequent injections of higher-reactivity fuel charges are then made, and these preferably distribute the higher-reactivity matter within the lower-reactivity chamber space such that combustion begins in the higher-reactivity regions, and with the lower-reactivity regions following thereafter. By appropriately choosing the reactivities of the charges, their relative amounts, and their timing, combustion can be tailored to achieve optimal power output (and thus fuel efficiency), at controlled temperatures (and thus controlled NOx), and with controlled equivalence ratios (and thus controlled soot).

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1. A compression ignition combustion method for an internal combustion engine, the method including the steps of: a. providing an initial fuel charge to a combustion chamber sufficiently prior to Top Dead Center (TDC) that the initial fuel charge is at least substantially homogeneously dispersed wit

1. A compression ignition combustion method for an internal combustion engine, the method including the steps of: a. providing an initial fuel charge to a combustion chamber sufficiently prior to Top Dead Center (TDC) that the initial fuel charge is at least substantially homogeneously dispersed within the combustion chamber by a time halfway through a compression stroke;b. providing a subsequent fuel charge to the combustion chamber at 40 or more degrees prior to Top Dead Center (TDC): (1) wherein the subsequent fuel charge and initial fuel charge have different reactivities, and(2) such that the subsequent fuel charge defines a volume within the combustion chamber having different reactivity than the remainder of the combustion chamber; andc. compressing the fuel charges until ignition occurs before the subsequent fuel charge can homogeneously disperse within the combustion chamber. 2. The method of claim 1 further including the step of providing exhaust gas from the combustion chamber back to the combustion chamber prior to or during the provision of the initial fuel charge to the combustion chamber. 3. The method of claim 1 wherein ignition results in: a. engine net indicated thermal efficiency of greater than 48%, andb. engine gross indicated thermal efficiency of greater than 51%. 4. The method of claim 1 wherein combustion products resulting from ignition provide: a. NOx emissions of less than 1.0 g/kW-hr, andb. soot emissions of less than 0.1 g/kW-hr. 5. The method of claim 1 wherein ignition results in peak cylinder pressure at or after Top Dead Center (TDC). 6. The method of claim 1 wherein ignition results in peak cylinder pressure between 5 and 15 degrees after Top Dead Center (TDC). 7. The method of claim 1 wherein ignition results in CA50 between approximately 0 to 20 degrees after Top Dead Center (TDC). 8. The method of claim 1 wherein: a. one of the initial fuel charge and the subsequent fuel charge contains gasoline; andb. the other of the initial fuel charge and the subsequent fuel charge contains diesel fuel. 9. The method of claim 1 wherein: a. one of the initial fuel charge and the subsequent fuel charge contains a first fuel; andb. the other of the initial fuel charge and the subsequent fuel charge contains a mixture of the first fuel and an additive. 10. The method of claim 1: a. wherein at least one of the initial and subsequent fuel charges includes a fuel provided to the combustion chamber from a tank, with the tank and the combustion chamber being situated within a vehicle;b. further including the step of: (1) altering the composition of the fuel between the tank and the combustion chamber to thereby alter the reactivity of the fuel,(2) without addition of any additive to the fuel. 11. The method of claim 1 wherein the initial and subsequent fuel charges enter the combustion chamber at different locations. 12. The method of claim 11 wherein: a. the initial fuel charge is supplied into the combustion chamber through an intake port;b. the subsequent fuel charge is supplied into the combustion chamber via direct injection. 13. The method of claim 1 wherein the initial fuel charge has a lower reactivity than the subsequent fuel charge. 14. The method of claim 1 wherein: a. Two or more subsequent fuel changes are supplied into the combustion chamber, andb. The subsequent fuel charges are introduced into the combustion chamber at different times. 15. The method of claim 14 wherein the subsequent fuel charges include: a. a first subsequent fuel charge provided to the combustion chamber between: (1) the closing of an intake port opening onto the combustion chamber, and(2) approximately 40 degrees prior to top dead center; andb. a second subsequent fuel charge provided to the combustion chamber after the first subsequent fuel charge. 16. The method of claim 14 wherein the subsequent fuel charges include: a. a first subsequent fuel charge, wherein at least a major portion of the first subsequent fuel charge is injected toward an outer region located at or near an outer radius of a piston face which partially bounds the combustion chamber;b. a second subsequent fuel charge supplied into the combustion chamber after the first subsequent fuel charge, wherein at least a major portion of the second subsequent fuel charge is injected toward an inner region spaced inwardly from the outer radius of the piston face. 17. The method of claim 14 wherein the subsequent fuel charges include: a. a first subsequent fuel charge, wherein at least a major portion of the first subsequent fuel charge is injected toward a region located outside of an outer third of the radius of a piston face which partially bounds the combustion chamber;b. a second subsequent fuel charge supplied into the combustion chamber after the first subsequent fuel charge, wherein at least a major portion of the second subsequent fuel charge is injected toward a region located inside an outer fourth of the radius of the piston face. 18. A compression ignition combustion method for an internal combustion engine, the method including the steps of: a. generating a fuel-air mixture within a combustion chamber wherein the mixture has a stratified distribution of fuel reactivity, with the mixture including: (1) an at least substantially homogeneous matrix of air and a first fuel, and(2) a second fuel situated within a sub-volume of the matrix, wherein the first and second fuel have different reactivities;prior to the latter half of the engine's compression stroke,b. compressing the fuel-air mixture until it ignites. 19. The method of claim 18 wherein the fuel-air mixture includes exhaust gas from a previously-ignited fuel-air mixture. 20. The method of claim 18 wherein ignition results in: a. engine net indicated thermal efficiency of greater than 48%, andb. engine gross indicated thermal efficiency of greater than 51%. 21. The method of claim 18 wherein combustion products resulting from ignition provide: a. NOx emissions of less than 1.0 g/kW-hr, andb. soot emissions of less than 0.1 g/kW-hr. 22. The method of claim 18 wherein ignition results in peak cylinder pressure at or after Top Dead Center (TDC). 23. The method of claim 18 wherein ignition results in peak cylinder pressure between 5 and 15 degrees after Top Dead Center (TDC). 24. The method of claim 18 wherein ignition results in CA50 between approximately 0 to 20 degrees after Top Dead Center (TDC). 25. The method of claim 18 wherein: a. one of the first fuel and the second fuel contains gasoline; andb. the other of the first fuel and the second fuel contains diesel fuel. 26. The method of claim 18 wherein: a. the first fuel contains the second fuel and an additive, orb. the second fuel contains the first fuel and an additive. 27. The method of claim 18 wherein the first and second fuels enter the combustion chamber at different locations. 28. The method of claim 18 wherein the first fuel has a lower reactivity than the second fuel. 29. A compression ignition internal combustion engine including: a. a combustion chamber;b. a first fuel supply bearing a first combustible material;c. a second fuel supply bearing a second combustible material, wherein the first and second combustible materials have different reactivity;d. a control system configured to: (1) provide an initial fuel charge to the combustion chamber from the first fuel supply prior to the latter half of the engine's compression stroke, to define an at least substantially homogeneous matrix of air and the initial fuel charge within the combustion chamber;(2) thereafter provide a subsequent fuel charge to the combustion chamber from the second fuel supply prior to the latter half of the engine's compression stroke, with the subsequent fuel charge defining a volume within the matrix having different reactivity than the remainder of the matrix; and(3) compress the matrix until ignition occurs. 30. The engine of claim 29 further including an exhaust system receiving exhaust gas from the combustion chamber, wherein a portion of the exhaust gas from the exhaust system is supplied back to the combustion chamber. 31. The engine of claim 29 wherein ignition provides: a. engine net indicated thermal efficiency of greater than 48%, andb. engine gross indicated thermal efficiency of greater than 51%. 32. The engine of claim 29 wherein combustion products resulting from ignition provide: a. NOx emissions of less than 1.0 g/kW-hr, andb. soot emissions of less than 0.1 g/kW-hr. 33. The engine of claim 29 wherein ignition results in peak pressure within the combustion chamber at or after Top Dead Center (TDC). 34. The engine of claim 29 wherein ignition results in peak pressure within the combustion chamber between 5 and 15 degrees after Top Dead Center (TDC). 35. The engine of claim 29 wherein ignition results in CA50 between approximately 0 to 20 degrees after Top Dead Center (TDC). 36. The engine of claim 29 wherein: a. one of the initial fuel charge and the subsequent fuel charge contains gasoline; andb. the other of the initial fuel charge and the subsequent fuel charge contains diesel fuel. 37. The engine of claim 29 wherein: a. one of the initial fuel charge and the subsequent fuel charge contains a first fuel; andb. the other of the initial fuel charge and the subsequent fuel charge contains a mixture of the first fuel and an additive. 38. The method of claim 29: a. wherein: (1) at least one of the first combustible material and the second combustible material include a fuel supplied from a tank;(2) the tank and the combustion chamber are situated within a vehicle;b. further including the step of: (1) altering the composition of the fuel between the tank and the combustion chamber to thereby alter the reactivity of the fuel,(2) without addition of any additive to the fuel. 39. The engine of claim 29 wherein the initial and subsequent fuel charges enter the combustion chamber at different locations. 40. The method of claim 39 wherein: a. the initial fuel charge enters the combustion chamber through an intake port;b. the subsequent fuel charge enters the combustion chamber via an injector. 41. The engine of claim 29 wherein the initial fuel charge has a lower reactivity than the subsequent fuel charge. 42. The engine of claim 29 wherein the control system is configured to provide two or more subsequent fuel charges to the combustion chamber at different times. 43. The engine of claim 42 wherein the subsequent fuel charges include: a. a first subsequent fuel charge provided to the combustion chamber following the closing of an intake port opening onto the combustion chamber, andb. a second subsequent fuel charge provided to the combustion chamber after the first subsequent fuel charge. 44. The engine of claim 42 wherein the subsequent fuel charges include: a. a first subsequent fuel charge, wherein at least a major portion of the first subsequent fuel charge is injected toward an outer region located at or near an outer radius of a piston face which partially bounds the combustion chamber;b. a second subsequent fuel charge supplied into the combustion chamber after the first subsequent fuel charge, wherein at least a major portion of the second subsequent fuel charge is injected toward an inner region spaced inwardly from the outer radius of the piston face. 45. The engine of claim 42 wherein the subsequent fuel charges include: a. a first subsequent fuel charge, wherein at least a major portion of the first subsequent fuel charge is injected toward a region located outside of an outer third of the radius of a piston face which partially bounds the combustion chamber;b. a second subsequent fuel charge supplied into the combustion chamber after the first subsequent fuel charge, wherein at least a major portion of the second subsequent fuel charge is injected toward a region located inside an outer fourth of the radius of the piston face.